TY - JOUR
T1 - Effects of initial mixture temperature and pressure on laminar burning velocity and Markstein length of ammonia/air premixed laminar flames
AU - Kanoshima, Ryuhei
AU - Hayakawa, Akihiro
AU - Kudo, Takahiro
AU - Okafor, Ekenechukwu C.
AU - Colson, Sophie
AU - Ichikawa, Akinori
AU - Kudo, Taku
AU - Kobayashi, Hideaki
N1 - Funding Information:
The present study was supported in part by the Council for Science, Technology and Innovation (CSTI), the Cross-ministerial Strategic Innovation Promotion Program (SIP), “Energy Carriers” (Funding Agency: The Japan Science and Technology Agency (JST)), the collaborative research project, Institute of Fluid Science, Tohoku University, and JSPS Grant-in-Aid for Scientific Research (B) (Project code: 20H02078).
Publisher Copyright:
© 2021 Elsevier Ltd
PY - 2022/2/15
Y1 - 2022/2/15
N2 - Ammonia is attractive not only as a hydrogen energy carrier but also as a carbon-free fuel. The goal of the present work is to study the laminar burning velocities and Markstein lengths of ammonia/air under a broad range of conditions including high-temperature and high-pressure because high-temperature and high-pressure conditions are relevant in internal combustion engines. The experiments were conducted in a constant volume chamber for equivalence ratios ranging from 0.8 to 1.2, initial mixture temperatures of 400 and 500 K, and initial mixture pressures ranging from 0.1 to 0.5 MPa. The temperature and pressure exponents were experimentally obtained, and it was clarified that the temperature exponents of the ammonia/air flame were larger than those of the methane/air flame. To evaluate the temperature and pressure effects on ammonia/air flames, these effects were compared with the effects on methane/air flames. Numerical simulations using the detailed reaction mechanisms showed that the effect of the initial mixture temperature on the reaction rate of H + O2 = O + OH was larger for ammonia/air flames than that for methane/air flames. This could be related to the difference in the effects of initial mixture temperature on the H2 and H radical formation reactions. The results also show that the pressure exponent of the ammonia/air flame was closer to zero compared with that of the methane/air flame. This observation can be explained from the standpoint of the effects of pressure on the reaction path of ammonia flames.
AB - Ammonia is attractive not only as a hydrogen energy carrier but also as a carbon-free fuel. The goal of the present work is to study the laminar burning velocities and Markstein lengths of ammonia/air under a broad range of conditions including high-temperature and high-pressure because high-temperature and high-pressure conditions are relevant in internal combustion engines. The experiments were conducted in a constant volume chamber for equivalence ratios ranging from 0.8 to 1.2, initial mixture temperatures of 400 and 500 K, and initial mixture pressures ranging from 0.1 to 0.5 MPa. The temperature and pressure exponents were experimentally obtained, and it was clarified that the temperature exponents of the ammonia/air flame were larger than those of the methane/air flame. To evaluate the temperature and pressure effects on ammonia/air flames, these effects were compared with the effects on methane/air flames. Numerical simulations using the detailed reaction mechanisms showed that the effect of the initial mixture temperature on the reaction rate of H + O2 = O + OH was larger for ammonia/air flames than that for methane/air flames. This could be related to the difference in the effects of initial mixture temperature on the H2 and H radical formation reactions. The results also show that the pressure exponent of the ammonia/air flame was closer to zero compared with that of the methane/air flame. This observation can be explained from the standpoint of the effects of pressure on the reaction path of ammonia flames.
UR - http://www.scopus.com/inward/record.url?scp=85118838975&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85118838975&partnerID=8YFLogxK
U2 - 10.1016/j.fuel.2021.122149
DO - 10.1016/j.fuel.2021.122149
M3 - Article
AN - SCOPUS:85118838975
VL - 310
JO - Fuel
JF - Fuel
SN - 0016-2361
M1 - 122149
ER -